View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 50U 60009B 24262.50337208 -.00000022 00000-0 58642-3 0 9997
2 50 47.2339 337.9389 0113800 277.0142 81.7717 12.20145473860412
| Epoch (UTC): | 18 September 2024 12:04:51 |
| Eccentricity: | 0.0113800 |
| inclination: | 47.2339° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 337.9389° |
| argument of perigee: | 277.0142° |
| revolutions per day: | 12.20145473 |
| mean anomaly at epoch: | 81.7717° |
| orbit number at epoch: | 86041 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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